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Analysis of an Application where the Unscented Kalman Filter is not Appropriate
(2009-09-15)
In this work a spin stabilized rocket with a ring of lateral pulse jets for attitude correction
and fins that open early in flight is simulated. The rocket is simulated with five different sensor
packages: rate gyros ...
Design, Testing, and Simulation of a Low-Cost, Light-Weight, Low-g IMU for the Navigation of an Indoor Blimp
(2008-09-09)
In this thesis we develop an IMU for the purpose of navigating an autonomous indoor blimp. Due to the unique system properties of an indoor blimp, the developed IMU is light-weight and is capable of measuring slow rotational ...